Zero clearance pinned structural connection

ABSTRACT

In a double layer grid-type of spare frame, certain straight framing members are connected at their opposite ends to separate node connectors carried by chords of the frame. The node connectors have elements which define a pair of spaced, parallel, substantially flat opposing surfaces. The framing members have substantially flat parallel opposing exterior surfaces at their ends which are disposed between the flat opposing surfaces of the node connectors. A shear pin passage is formed through each framing member and on a line normal to the end&#39;s parallel exterior surfaces. Holes for a shear pin are formed through the node connector elements on a line normal to the elements&#39; opposing surfaces. A shear pin is engaged in the element holes and the framing member pin passage to define a pinned connection of the framing member to the node connector. In each connection, the pin diameter, the passage diameter, and the hole diameters are coordinated so that the pin has an essentially interference fit in the passage and in the holes.

CROSS-REFERENCE TO RELATED APPLICATION

This application is a division under 35 U.S.C. § 120 of co-pendingapplication Ser. No. 11/525,721 filed Sep. 22, 2006, and claims thepriority of only that Application and not the priority of anyapplication filed before application Ser. No. 11/525,721.

FIELD OF INVENTION

This invention pertains to pinned connections in structural spaceframes. More particularly, it pertains to a connection in which there isessentially zero clearance between a pin and the elements connected bythe pin.

BACKGROUND OF THE INVENTION

A space frame is a network of structural framing members, such as tubes,interconnected at multi-member connection points (commonly called“nodes”) in such a way that the whole structure behaves as onestructural element. By contrast, in the typical framing of beams andcolumns, as in buildings, structural elements often act independently ofeach other and can have completely separate force paths.

Two broad classes of space frames are recognized in the art. They aresingle layer grids and double (multiple) layer grids (DLGs). A singlelayer grid is a network (arranged on a triangular, rectangular or othergeometric scheme) of node structures and structural members of desiredcross-sections and sizes. A single layer grid achieves its structuralstrength by locating the grid elements in a curved surface. Thus, singlelayer grids are most commonly used to define domes, vaults, and otherconstructions having simple or compound curvature.

Double layer grids, as the name implies, are space frames in which thenodes are located in two separate surfaces which commonly are flat andin parallel spaced relation to each other; vaulted DLGs having curvedparallel spaced surfaces also are known. In a double layer grid (DLG),the nodes are interconnected in each surface by straight structuralelements called chords; the chords in each surface are arranged inrepeating geometric patterns which usually are squares, but trianglesand rectangles also can be defined by the chord array in each surface.The squares (or other geometric shapes) defined by the chords in theprincipal surfaces of a DLG normally are of the same size throughout thestructures. The two surfaces of a DLG are interconnected by furtherstraight structural elements which are referred to herein as struts todistinguish them from the chord elements which lie in the principalsurfaces of a DLG. The nodes in a top surface of a DLG are located sothat the centroid of the area of the square, e.g., they define islocated over a node in the bottom surface of the DLG, and struts areconnected from each of those top surface nodes to that bottom surfacenode. As a result, the struts in a DLG which extend between theprincipal surfaces of the DLG are oblique to the principal surfaces.

Space frames are routinely used as static structures, i.e., structureswhich are mounted on and supported by fixed supports or foundations. DLGstructures which are square or rectangular in overall plan view (i.e.,as seen from a vantage point on a line perpendicular to the DLGsprincipal surfaces) can be supported at the ends of the structure or atthe mid-length, e.g., of the structure. However, it is known to usespace frames as movable covers over sports arenas and stadiums, in whichcase the space frame supports are carried on roller or trolley unitswhich are movable along horizontal tracks; space frames used in suchsituations are fundamentally static structures because the movement ofsuch a space frame does not significantly alter the frame loads due togravity.

The connections of framing members to nodes in a single layer gridrarely are anything other than rigid connections defined by bolting,riveting or welding of the associated framing members to each other orto other node elements at a node. Such rigid connections of framingmembers at grid nodes enables the connections to transmit to the nodes,and to other members at the node, moment loads on the framing members;moment loads are loads which act on a framing member in ways which causethe framing member to tend to rotate or pivot relative to the node. Inmodern double layer grids, on the other hand, the connections of theframing members to the nodes rarely are moment connections; they areconnections which either are true pinned connections or are connectionswhich are modeled as pinned connections. In a double layer grid, loadson the overall grid which would tend to produce rotational movements offraming members relative to the nodes are resisted by tensile orcompressive forces which act in the framing members along their lengths,i.e., axially of the framing members. The reason for the use of pinnedconnections in DLGs is the cost and difficulty of assembling such gridshaving moment connections of the framing members at or to the nodes.

A true pinned connection of a DLG framing member at a node is a simpleconnection to define and to make. Such a connection typically is made bypassing a bolt or a pin through aligned holes in a framing member and ina node connector arrangement to which that framing member and otherframing members are pinned. To the extent that strut axes do notintersect the axes of the chords at the node (or the axis of a majorchord at the node), the node is said to have eccentricity. Eccentricityat a DLG node causes the node to have moment loads or other undesiredloads applied to it. The presence of moment loads at nodes of a DLGrequires that at least some of the components of the grid be heavierthan if no moment loads were present. Load eccentricity at a DLG nodecan be caused by imperfections in the alignments of the framing membercoupled to the node, and framing member misalignments can be produced byclearances in the pinned connections at the node. Clearances at pinnedconnections in a DLG also can cause the grid framing members to haveeffective lengths between nodes which deviate from design lengths,thereby affecting the magnitudes of the actual loads in the framingmembers as compared to design load magnitudes. The solution to theexistence of (or potential for) differences between actual and designframing member loads is to make the framing members heavier.

It is apparent, therefore, that existing structures and techniques forestablishing connections of framing members to nodes in DLGs havedeficiencies which adversely affect the load carrying capacities of anoverall DLG and of the framing members present in it. Needs exist forstructures and procedures by which pinned connections at nodes in DLGscan be made with reduced or no eccentricity and with minimal effects ofclearances at the pinned connections. Meaningful satisfaction of any orall those needs can result in DLGs which make more efficient use oftheir framing members and so permit weights of framing members to bereduced, along with other consequent benefits and advantages. Theprincipal factors effecting the cost of a given DLG are primarily thecost of the materials used to define the grid components and secondarilythe cost of labor to assemble those components. Material cost is afunction of material weight. Labor costs are a function principally ofthe man-hours needed to assemble a DLG.

SUMMARY OF THE INVENTION

The invention beneficially addresses the needs identified above. It doesso by providing structural arrangements and are procedures whichdescribed in detail below, along with descriptions of the severalbenefits and advantages of those structures and procedures. Principalaspects of the invention as claimed are summarized next below.

Not used.

This invention provides a pinned connection of an end of a framingmember in a double layer grid-type of space frame at a node of the framevia a node connector having elements which define a pair of sparedparallel substantially flat opposing surfaces. The framing member end isdisposed between the opposing element surfaces of the node connector andhas, its own substantially flat and substantially parallel oppositeexterior surfaces which. A pin receiving passage is formed through theframing member along a line which is substantially normal to the framingmember's parallel exterior surfaces. A pair of holes are formed throughthe node connector elements on a line substantially normal to the pairof opposing surfaces defined by those elements. A pin is insertablethrough the holes and the passage upon suitable placement of the framingmember and between the opposing surfaces of the node connector. In thatcontext, the pin is defined to have substantially an interference fitwithin the holes and the passage upon insertion of the pin into theholes and the passage.

Not used.

Not used.

BRIEF DESCRIPTION OF THE DRAWINGS

The previously mentioned and other aspects of this invention, andbenefits, features and advantages of them, are more fully described andnoted in the following detailed descriptions made with reference tocertain structural and procedural embodiments of the invention which aredepicted in the accompanying drawings in which:

FIG. 1 is a perspective view of a double layer grid (DLG) space frame ofindeterminate length and which has constant square bay spacing;

FIG. 2 is a perspective of a simple DLG space frame, in the nature of atriangular truss, which has variable bay spacing;

FIG. 3 is a perspective view of a node connector for the space frameshown in FIG. 2;

FIG. 4 is a fragmentary end elevation view of the node connector of FIG.3 with connections of framing members to it in the construction of thespace frame shown in FIG. 2;

FIG. 5 is an end elevation view of a more complex DLG space frame whichis a movable support armature for a curved mirror and is useful in asolar power generation installation;

FIG. 6 is an end view of a first node connector configuration useful inthe DLG shown in FIG. 5;

FIG. 7 is a perspective view of the node connector of FIG. 6;

FIG. 8 is an end view of a second node connector configuration useful inthe DLG shown in FIG. 5;

FIG. 9 is a perspective view of the node connector of FIG. 8;

FIG. 10 is an end view of a third node connector configuration useful inthe DLG shown in FIG. 5;

FIG. 11 is an elevation view of a shear pin useful in making connectionsof space frame framing members to node connectors in the practice ofaspects of this invention;

FIG. 12 is a plan view of a known style of clip retainer useful with theshear pin of FIG. 11;

FIG. 13 is a perspective view illustrating a first step in theconstruction of the DLG of FIG. 5;

FIG. 14 is a perspective view illustrating a second step in that sameconstruction process;

FIG. 15 is a perspective view illustrating a third step in that sameconstruction process;

FIG. 16 is a perspective view illustrating a fourth step in that sameconstruction process;

FIG. 17 is a perspective view illustrating a fifth step in that sameconstruction process;

FIG. 18 is a perspective view illustrating a sixth step in that sameconstruction process;

FIG. 19 is a perspective view illustrating a seventh step in that sameconstruction process;

FIG. 20 is a perspective view illustrating an eighth step in that sameconstruction process;

FIG. 21 is a perspective view illustrating a ninth step in that sameconstruction process;

FIG. 22 is a perspective view illustrating a tenth step in that sameconstruction process, substantial parts of the previously assembledspace frame being deleted from FIG. 22 for enhanced clarity of depictionof structure being added by step ten;

FIG. 23 is a top plan view which illustrates an eleventh step in thatsame construction process;

FIG. 24 is a fragmentary end elevation view of a portion of thestructure shown in FIG. 23;

FIG. 25 is a perspective view of one of the two pivot (torque transfer)arms which are components of the mirror support armature of FIG. 5;

FIG. 26 is an elevation view of another shear pin useful in the practiceof aspects of this invention;

FIG. 27 is a cross-sectional elevation view of a DLG framing memberaccording to an aspect of the invention;

FIG. 28 is a cross-sectional elevation view of another DLG framingmember which uses the same design principles on the framing member shownin FIG. 27;

FIG. 29 is a cross-sectional view of another node connector according tothe invention in which the connector's chord receiving passage is notfully closed but is sufficiently closed that the cooperation of theconnector with a chord inserted axially into it holds the chord so thatits axis is aligned with the passage axis and the chord can move onlyaxially in the passage;

FIG. 30 is a cross-section view of a further node connector which is avariant of the node connector shown in FIG. 29, the variation being thatthe node connector is defined by two identical parts, which preferablyare extrusions, secured to each other and to a frame chord;

FIG. 31 is a cross-section view of a still further node connectoraccording to the invention which is a variant of the node connectorshown in FIG. 30 and in which the chord includes an external radial ribthrough which passes a bolt securing the connector parts to each otherand to the chord;

FIG. 32 is a schematic plan view of a “free form” DLG space frame whichcan be constructed using node connectors according to this invention;and

FIG. 33 is an elevation view taken along line 33-33 of FIG. 32.

DETAILED DESCRIPTION OF THE INVENTION

FIG. 1 is a perspective view of a portion of a rectilinearly subdividedDLG space frame 10. Frame 10 is composed of framing members which aredisposed to define top 11 and bottom 12 layers of the frame and tointerconnect those layers in an arrangement which causes frame layers 11and 12 to be in spaced parallel relation to each other. Layers 11 and 12can also be called grids, hence the name double layer grid (DLG) for thetype of space frame shown in FIG. 1.

The framing members of DLG 10 are comprised by chords which areinterconnected to define top and bottom layers 11 and 12 of the DLGwhich has an end 13 and opposite sides 14 and 15. The chords whichextend along the length of the DLG can be and preferably are continuous(subject to limitations on the lengths available) and, for presentpurposes, are called major chords. Thus, DLG 10 includes upper majorchords 16 and lower major chords 17. In each layer of DLG 10, the upperand lower major chords are interconnected and spaced by upper 18 andlower 19 transverse minor chords, each of which has a length equal (oressentially so) to the spacing between the major chords which theyinterconnect. The major and minor chords of DLG 10 are aligned to beparallel to respective orthogonal directions, i.e., the length and thewidth, of the DLG. In each layer, the major and minor chords areinterconnected at junction points which are commonly called nodes. Thus,DLG 10 has upper nodes 20 and lower nodes 21. As is common in DLG, thedistance in each layer between adjacent parallel minor chords is equalto the distance between adjacent parallel major chords, and so the uppernodes 20 and the lower nodes 21 are located at the corners of alignedrows and columns of squares bounded by the major and minor chords; eachtop layer square corresponds to a bay of the DLG; the chords in thebottom layer of frame 10 also define square bays. Thus, consistent withthe foregoing, DLG 10 has constant square bay spacing.

If the spacing between adjacent parallel minor chords of a DLG is moreor less than the spacing between adjacent major chords in a layer, theDLG is described as having constant rectangular bay spacing.

Chords 16 and 18 of DLG 10 can be said to be in (or to define) a topsurface of the DLG; similarly, chords 17 and 19 are in (define) a bottomsurface of the DLG. The top and bottom surfaces of DLG 10 are parallel.

The top and bottom layers of DLG 10 are spaced from and supportedrelative to each other by further diagonal framing members 22 calledstruts each of which extends between a top layer node 20 and a bottomlayer node 21. In order that the upper and lower grids may be stifflyfixed relative to each other by the struts, the upper major and minorchords are offset relative to the lower major and minor chords in suchmanner that the lower nodes 21 are located vertically below the centersof the square openings defined by the chords of the upper grid; uppernodes 20 are located vertically above the centers of the openingsdefined by the chords of the lower grid. Thus, the struts are disposedin planes which are inclined relative to the top and bottom surfaces offrame 10. As shown in FIG. 1, within the boundaries of the frame, thereare four struts 22 connected to each upper node 20 and to each lowernode 21. As a result, the struts are disposed in two sets of parallelplanes, one set parallel to and intersecting one upper major chord andone lower major chord, and one set parallel to and intersecting one lineof upper minor chords and one line of lower minor chords. Along the endsand sides of frame 10, there are two struts 22 connected to each uppernode 20, and the frame end and side surfaces (strut planes) slope downand inwardly between the top and bottom surfaces of the frame.

In the classic frame 10 shown in FIG. 1, there are fewer squares inbottom layer 12 than there are in top layer 11. As frame 10 is depictedin FIG. 1, the frame is six squares (bays) wide in its top layer andfive squares (bays) wide in its bottom layer, while the length of theframe as depicted is indefinite. Such a DLG frame can be described bythe notation 6×n/5×(n−1) in which 6×n denotes a top grid 6 bays wide byn bays long, and the notation 5×(n−1) denotes a bottom grid 5 bays wideby (n−1) bays long.

The description of frame 10 to this point has pertained to geometricalaspects of the frame, to the linear structural framing members whichcomprise the frame, and to the nodes where the lines (axes) of thedifferent framing members intersect each other in an ideal frame. Thatdescription is a background and foundation for the followingdescriptions of actual frames and of the structures which are employedto interconnect framing members at nodes in those frames. The followingdescriptions include descriptions of node connector arrangements whichenable the design and construction of DLG-type space frames havingadvanced properties and benefits.

FIG. 2 is a perspective view of a DLG-type space frame 25 in the form ofa truss of inverted equilateral triangular cross-section. Using thenotation described above, frame 25 is a 1×8/0×0 DLG frame. Frame 25 hastwo upper major chords 26 and one lower major chord 27, all of whichextend along the full length of the frame.

FIGS. 3 and 4 show a node connector 28 of frame 25. Because thecross-sectional configuration of frame 25 is that of an equilateraltriangle, a single basic node connector configuration can be used at allnodes in the frame. The framing members of frame 25 preferably aresquare tubes, the major chords preferably having cross-sections largerthan the cross-sections of the other framing members (minor chords,struts, and torsion braces) present in the frame; the other framingmembers preferably are of the same cross-sectional dimensions. The framematerial preferably is an extrudible aluminum alloy, and the framingmembers preferably are extruded aluminum tubes. Also, the nodeconnectors 28 preferably are defined by extrusions of the same aluminumalloy.

FIG. 4 shows the pinned connection of two struts 30 to a node connector28 which has a pinned connection to lower chord 27; a connection ofstruts to a node connector on either of the upper major chords wouldhave substantially the same appearance as shown in FIG. 4 except thatthe upper major chords actually are turned about their longitudinalaxes—visualize that FIG. 4 is rotated 60° in either direction.

Node connector 28 has a chord-receiving base channel portion 31 whichhas a flat base 32 and two parallel spaced flanges 33 perpendicular tothe base. The spacing between opposing faces of flanges 33 is slightlygreater than the exterior width of a major chord, and the height of theflanges from the base 31 preferably is equal to the height of a majorchord. Node connector 28 also carries along the exterior of the channelportion, in directions parallel to the length of the connector's channelportion, plural fixed structural elements (flanges or ribs) 34 whichdefine two pairs of parallel spaced opposing and substantially flatsurfaces 35 and 36. Surfaces 35 and surfaces 36 are spaced a distancewhich is slightly greater than the width of the extrusion from which thestruts, minor chords and torsion braces of frame 25 are defined.Further, surfaces 35 are spaced parallel to and equally from oppositesides of a plane 37 which passes through the structural neutral axis ofbottom chord 27 as received in and secured in the channel portion 31 ofnode connector 28 as shown in FIG. 4. Because chord 27 is defined by anextruded square tube of uniform wall thickness, the location of theneutral axis of the chord is coincident with the centroid of thecross-sectional area of the tubular chord. Similarly, surfaces 36 arespaced parallel to and equally from opposite sides of a plane 38 whichpasses through the neutral axis of chord 27 as received and secured innode connector 28. Thus, regardless of the angularity of a strut 30, aspinned to the node connector, relative to the length of the nodeconnector, axial forces (tensile or compressive) in the truss arealigned with and pass through the neutral axis of the chord to which thenode connector is fixedly (rigidly) mounted as by the use of shear pins.That is, because flanges 34 are parallel to the length of the nodeconnector and have the described geometrical relations to the channelportion of the node connector, the assembled node connection is free ofeccentricities regardless of the angularities of the pertinent strutsrelative to the chord.

Node connector 28 preferably is doubly pinned to chord 27 by use ofshear pins 40 and clip retainers 41 as depicted in FIGS. 11 and 12.Double pinning of the connector to chord 27 provides a rigid connectionbetween them; in a DLG a rigid connection of a node connector to atleast one of the framing members engaging that node connector isimportant. To enable the node connector 28 to be doubly pinned to chord27, the connector has two sets of shear pin holes 42 formed throughchannel portions flanges 33 at spaced locations along the length of theconnector. The two holes 42 in each hole set are centered on a linewhich is normal to the length of the node connector and passes throughthe neutral axis of the chord 27 as secured in node connector. Similarshear pin holes are formed through the walls of chord 27 on a lineperpendicular to the chord's length and passing, preferably, through theneutral axis of the chord. If the length of truss 10 exceeds the lengthat which chords 26 and 27 can be obtained or conveniently handled, nodeconnectors 28 can be used to make splices between aligned chord memberlengths. Splicing is accomplished by making a splicing node connector ofextended length, and by doubly pinning the adjacent ends of two chordmember lengths to the node connector.

In like manner, shear pin holes 43 are formed through node connectorflanges 34 for each other framing member which is to be connected tothat node connector in completed frame 25. In this instance, becauseeach other framing member is simply (singly) pinned to the nodeconnector, one hole 43 per each framing member to be connected to theconnector is formed in each relevant flange 34, and the two holes in thecoacting flanges are centered on a line which is perpendicular to flangesurfaces 35 or 36. Similarly, two aligned shear pin holes are formedthrough the walls of each other framing member; they are located on aline perpendicular to the length of the framing member and passing,preferably, through the neutral axis of that member.

As shown in FIG. 2, upper major chords 26 and lower chord 27 of frame 25are of equal length; compare the different lengths of major chords 16and 17 in frame 10 shown in FIG. 1. Upper major chords 26 are located inspaced parallel relation to each other by minor chords 44 which areparallel to each other and perpendicular to the major chords, and so theupper major chords mount (as described above) node connectors 28 attheir ends and at opposed locations spaced along their lengths. Toafford connection points for the diagonal struts 30 in frame 10, nodeconnectors 28 are fixedly mounted to lower chord 27 at locations betweenthe ends of that chord which are, respectively, midway along thedistance between corresponding upper minor chords 44. Also, toaccommodate the mounting of frame support fittings 45 to the oppositeends of frame 25, an end node connector 28 is fixedly mounted to eachend of lower chord 27.

As to each of node connectors 28 located between, rather than at, theends of lower chord 27, four struts 30 are pinned to each connector; twoof those struts have their ends snugly yet movably received betweensurfaces 35 of the connector so that the opposing flat exterior surfacesof the strut substantially register with surfaces 35, and another two ofthose struts have their ends snugly yet moveably received betweensurfaces 36 of the connector so that the opposing flat exterior surfacesof those struts substantially register with surfaces 36. The ends ofstruts 30 are pinned to the connectors 28 with which they cooperate byuse of shear pins 40 passed through the strut-end holes and throughholes 43 of the connector. All shear pins are held in place byconnection of clip retainers 41 to the pins; each retainer cooperateswith its pin in a circumferential recess (groove) 47 defined in theround pin shank adjacent a distal end of the pin which is opposite froman enlarged head 48 at the other end of the pin. Two struts 30 areconnected from the node connector at each end of lower chord 27 to acorresponding frame end connector at the adjacent ends of upper majorchords 26; see FIG. 2.

Further, to make frame 25 stiff against torsional or wracking loadsimposed upon it in use, frame 25 includes a torsion brace framing member49 in each bay of the frame; a bay of frame 25 is the opening bounded bythe upper major chords 26 and two adjacent upper minor chords 44. Eachtorsion brace is connected between the node connectors at the diagonallyopposite corners of a bay. The torsion braces lie in the plane of theupper minor chords, and so the torsion brace ends are simply (singly)pinned between the same surfaces 35 or 36 of each affected nodeconnector between which an end of an upper minor chord 44 is similarlypinned. In the portion of frame 25 between its end bays, the torsionbraces 49 alternate in the directions in which they are skewed to thelength of the frame.

Attention is drawn to the node connectors denoted 28′ and 28″ in FIG. 2;they are at the opposite ends of a single upper minor chord 44. Inaddition to being associated with an upper major chord 26, connector 28′has associated with it two struts 30, an upper minor chord 44, and twotorsion braces 49. Struts 30 can be received between surfaces 35 ofconnector 28′ and framing members 44 (one) and 49 (two) can be receivedbetween surfaces 36 of that connector. By contrast, node connector 28″has associated with it an upper major chord, a minor chord 44, and twostruts 30. To accommodate those differences in the number of connectionsto them, connector 28′ has a length greater than that of connector 28″by an amount adequate to accommodate the ends of three framing membersbetween surfaces 36 of connector 28′. That connector length differenceis easily handled by making connector 28′ from a longer length of theconnector extrusion than the length of the extrusion section used madeconnector 28″, and by drilling three sets of holes 43 through theflanges forming surfaces 35 rather than one set of such holes.

It is a feature of frame 25 that all of the shear pin holes formed ineach node connector 28 have the same design diameter (and preferablyactual diameter) as the diameter of the cylindrical shanks of the shearpins to be inserted into those holes, and that the shear pin holesformed in all framing members of frame 25 also have the same design(also preferably actual) diameter as the shank diameter of the shearpins used to pin them to node connector 28. That is, each shear pin haszero clearance relative to the node connector and framing member holesthrough which its shank will be inserted to connect the relevant framingmember to the relevant node connector. Such zero clearance means, as apractical matter, that each shear pin has an interference fit in each ofthe holes with which it coacts when installed in the frame. Such zeroclearance of shear pins in connector and framing member holes means thatframe 25 can be built with great precision and has no play or loosenessin any of its connections. As noted above, the lack of play or loosenessin the framing member connections in a space frame means that eachframing member will experience and transmit loads which very closelycorrespond to design loads, and that all framing members willeffectively share and correctly transmit loads and load forces withinthe frame. There will be minimal instances of some framing memberscarrying more or less of the fraction of the total loads they weredesigned to carry. Consequently, lower safety factors can be used in thedesign of frame 25 and correspondingly lighter framing members can beused than if the frame connections have play or looseness, withoutcompromising safety or structural adequacy.

An inspection of FIG. 2 will reveal that it has 8 bays along its length,i.e., 8 intervals between 9 spaced upper minor chords 44. Suchinspection of FIG. 2 will reveal that the 4 bays in the mid-length ofthe frame are of the same length, which length is less than the equallengths of the other 4 bays of the frame. Thus, frame 25 has variablebay spacing; bay spacing in frame 25 can be defined as the distancealong the length of the frame between the centroids of the rectangularareas on opposite sides of a minor chord. Variable bay spacing meansthat some node connectors are closer to each other along a given majorchord than are others of the node connectors along that major chord.Because of the natures of the node connectors 28 as described above, allof the node connectors along that major chord can be (preferably are)made with the same transverse cross-sectional configuration, i.e., madeby use of different pieces cut from a single extrusion. Variable bayspacing is possible with node connectors 28 because, in all of the nodeconnectors, the elements of the connectors which define surfaces 35, 36are arranged to be parallel to the length of the portion of theconnector which cooperates with the major chord of the frame which can(preferably does) extend continuously through the connector. Variablebay spacing is easily achieved in frame 25 by varying the lengths ofstruts 30 and of torsion braces 49 as needed.

It is preferred that the node connectors and framing members of frame 25be defined of the same material so that they all have the samecoefficient of thermal expansion, thereby resulting in a frame whichdevelops minimal stresses in it with temperature change and does notdeflect or distort due to temperature changes. The preferred materialfor definition of the node connectors and framing members of frame 25 isan aluminum alloy, and those frame elements preferably are made byextrusion processes. Shear pins used in the connections within the framecan be made of aluminum or of stainless steel.

However, it is within the scope of this invention that the nodeconnectors and framing members of frame 25, or of other frames accordingto this invention, can be made of other materials. If steel is thematerial of choice, it will be apparent that the node connectors can befabricated out of discrete components preferably welded together intointegral articles of manufacture. Pultruded materials such as fiberreinforced plastics (synthetic resins) can be used; in that connection,pultruded components are regarded as equivalents of extruded components.Both extruded and pultruded components can be used in a given frameaccording to this invention. Node connectors can be made by otherfabrication processes such as casting or machining.

Regarding frame 25, it was noted that, because the overall cross-sectionconfiguration of the frame is that of an inverted equilateral triangle,all node connectors in the frame can have the same cross-sectionalconfiguration. If the frame cross-sectional configuration were that ofan isosceles triangle, then two different cross-sectional configurationswould be needed for the node connectors. Similarly, if the frameconfiguration were to be that of a triangle having no equal includedangles, three different node connector cross-sections would be required.The principles used in the design of node connectors 28 can be used inthe design of node connectors for DLG-type space frames having otherconfigurations than trusses of triangular cross-section. Square-sectionbox trusses can be defined by a variation of node connectors 28 in whichthe central planes between surfaces 35 and 36 intersect each other at a90° angle father than a 60° angle. Moreover, a truss designed andconstructed according to this invention can be disposed vertically toserve as a tower. Different node connector cross-sections are readilyaccommodated in the practice of this invention, as made more clear bythe following descriptions.

FIG. 5 is an end view of another space frame 50 according to thisinvention. Frame 50 is a double layer grid (DLG) frame which has a flatbottom surface defined by two bottom major chords 51, 52 and bottomminor chords 53 which extend transversely of those major chords. Theupper surface of frame 50 is not flat, but instead has the contour of ashallow V (oblique included angle) which is concave upwardly away fromthe frame's bottom surface; the frame is substantially symmetrical abouta bisector plane of that included angle. The upper surface is defined bytwo planes 54, 55 which intersect at the axis of an upper central majorchord 57. Two upper outer major chords 58, 59 are located equidistantlyfrom and on opposite sides of center chord 57 and lie, respectively, inplanes 54 and 55. Upper center major chord 57 is positioned centrallyabove and parallel to bottom major chords 51, 52 by central struts 60 ofequal length. Each of upper outer major chords 58, 59 is positionedrelative to the upper central major chord and to the adjacent bottommajor chord by upper minor chords 61 and by struts 62 which are longerthan central struts 60. The major chords of frame 50 preferably aredefined by round tubes. The minor chords, struts, torsion braces andauxiliary framing members (see the following descriptions) preferablyare defined by square tubes. The tubes (round and square) preferably aredefined by aluminum extrusions, as are all of the three different stylesof node connectors at which the framing members of frame 50 areinterconnected.

The intended use of frame 50 is as a movable support armature for anelongate preferably cylindrically curved mirror 64 in a solar powergeneration facility; the position of a mirror 64 relative to the frameis shown in FIG. 5. To enable the frame to serve in that capacity, theframe is designed and constructed to carry a mounting and torquetransmitting arm 65 at each of its ends, and to carry supports 66 fortubes through which a liquid is circulated to be heated by solarradiation reflected by the mirror. The complete mirror and mirrorsupport frame assembly has a center of gravity and a center of rotationwhich are coincident at 67 in arms 65.

In light of the foregoing descriptions of truss frame 25 and its nodeconnectors 28, it will be apparent that frame 50 includes three stylesof node connectors which cooperate respectively with bottom major chords51, 52, with upper center major chord 57, and with upper outer majorchords 58, 59. Those three styles of node connectors are shown,respectively, in FIGS. 6 and 7, in FIGS. 8 and 9, and in FIG. 10.

Bottom major chord node connectors 69 have the cross-sectionalconfiguration shown in FIG. 6. Unlike node connectors 28 in frame 25,node connectors 69 are configured for cooperation with a major chordframing member which is defined in the form of a round tube. A nodeconnector 69 has a brace circularly cylindrical chord engaging portion70 which defines a round circumferentially closed passage 71 whichextends along the length of the connector. The diameter of passage 71 isslightly greater than the outer diameters of the bottom major chords offrame 50 so that each connector enables a chord tube to be snugly andslidably inserted into and through the node connector. At least one pair(preferably two pairs) of holes 72, aligned on a diameter of passage 71,are formed through the connector's chord engaging portion to enableshear pins (preferably zero-clearance shear pins as described above) tobe used with cooperating holes in the pertinent major chord tube tofixedly mount the connector to the chord tube. In other respects,however, node connectors 69, as well as upper central node connectors 74(FIGS. 8 and 9) and upper outer chord node connectors 75 (FIG. 10) offrame 50, are sufficiently similar to node connectors 28 that, in viewof the content of FIGS. 6-10, extended descriptions of frame 50's nodeconnectors are not needed for an understanding of them by a personskilled in the art.

Therefore, briefly noted, each of major chord node connectors 69, 74 and75 carries along its length and externally of its tubular chord engagingbase portion 70 a plurality of fixed structural elements 77 which defineplural pairs of parallel spaced opposing substantially flat surfaces 78,79, 80 (FIG. 6 as to connector 69), 81, 82, 83, 84 (FIG. 8 as toconnector 74), and 85, 86 and 87 (FIG. 10 as to connector 75). Thefacing ones of surfaces 78-87 afford snug yet movable registration withoppositely facing flat exterior surfaces of the minor chords and otherframing members of frame 50 upon insertion of ends of those framingmembers between those facing surfaces as frame 50 is assembled (seeFIGS. 13-24). Aligned pairs of holes 89 are formed through elements(flanges) 77 at suitable locations in each particular node connector toenable the insertion of zero-clearance shear pins through them andthrough holes formed through the ends of the relevant framing members,as described above concerning frame 25.

FIGS. 6, 8 and 10 show that certain ones of flanges 77 can be branchedat their outer ends in order to define facing surface pairs 78-87 inwhich, in each pair, the surfaces are parallel to and equidistantly fromcorresponding central planes which include the axis of that nodeconnector's chord receiving passage 71 and the neutral axis of the roundtubular major chord received in that passage.

That is, in the node connector shown in FIG. 6, the connector elements77 which define adjacent ones of surfaces 78 and 79, and which defineadjacent one of surfaces 79 and 80, are not connected directly to theexterior of tube portion 70. Instead they are carried at the ends ofribs which are connected directly to the exterior of tube portion 70.The ribs preferably are disposed in planes which intersect the connectorpassage axis. This feature of a node connector allows connection to theconnector of framing members lying in planes which have relatively smallangular separation between them at the node connector while enabling theneutral axes of those framing members to have the desired intersectionwith the neutral axis of a framing member (chord, e.g.) located in thepassage 71 of that node connector. The movement of the shear pinlocations outwardly from the tube portion of the node connector is not adisadvantage.

The structure of completed frame 50 will become apparent from anunderstanding of FIGS. 13-24 which depict consecutive steps in theassembly of the frame from its component round and square tubularframing members and its node connectors 69, 74 and 75. The first ofthose steps is shown in FIG. 13. Node connectors 69 are engaged aroundthe preferably tubular round member which defines bottom major chord 52and are secured to it at the ends and the center of that chord. Eachprefabricated node connector of frame 50 can bear coding notations whichinform those persons assembling the frame where each node connector isto be placed in the frame and what directionality it is to have relativeto the ends of its major chord member. Then, as shown in FIG. 14, threenode connectors 69 are similarly engaged around and secured to bottommajor chord 51.

As shown in FIG. 15, a third step in the frame assembly process can bethe mounting of five node connectors 74 in the proper sequence on uppercenter major chord 57 and the pinning of them to the chord. In thatprocess, a plate 90 is mounted to the chord in association with thecentral node connector, which plate will later have connected to it asupport 66. Note that node connectors 74 are not uniformly spaced alongchord tube 57; see also FIG. 19 where the reason for that connectorspacing is made apparent. Fourth and fifth steps in the frame assemblyprocess can be the placement of node connectors 75 on each of outercentral major chord tubes 58 and 59 and the pinning of those connectorsto those tubes; see FIGS. 16 and 17.

FIG. 18 illustrates a sixth step in the frame assembly process, namely,the interconnection of bottom major chord tubes 51 and 52 by bottomminor chords 53, torsion bracing members 92 and additional elements ofthe frame, using zero-clearance shear pins to make all connections tonode connectors. The major chords 51, 52 and the minor chords 53 definetwo rectangular bays in the bottom layer (surface) of frame 50. Thosemajor chords are shorter in length than upper major chords 57-59.Compensation for that major chord length difference is achieved byconnecting to each end of each bottom major chord tube an additionalpreferably square framing member 93. At each end of the bottom layerassembly, the other ends of transversely adjacent members 93 are doublypin-connected or bolted (a stiff connection) to a coupling fitting 94 towhich an end of a frame torque arm 65 later will be secured.

The upper central major chord subassembly (FIG. 15) can be connected inplace relative to the bottom major chord assembly (FIG. 18) as depictedin FIG. 19 as a seventh step in the assembly process. Central struts 60are pinned between the node connectors 69 on the bottom major chords andthe end node connectors 74 on the central chord, and the two otherconnectors 74 which are on opposite sides of the center of upper centerchord 57. Two further framing members 95 are pinned between center nodeconnector 74 on upper chord 57 and the respective center node connectors69 on bottom chords 51, 52. Plate 90 can then be secured, as by boltingor riveting, to the ends of members 95 which are pinned to center nodeconnector 74. Plate 90 can be further fixed in its desired position byconnecting braces 96 between the central part of the plate and framingmembers 95 as shown in FIG. 19. The completion of this assembly stepcauses torque arm connection fittings 94 to be located substantiallybelow the opposite ends of upper central major chord 57.

Eighth and ninth steps in the assembly of frame 50 can be the pinnedconnection of upper outer major chords 59, 58 to bottom major chords 52,51, respectively, via longer struts 62 and node connectors 69 and 75.See FIGS. 20 and 21.

A tenth step in assembly of frame 50 can be the interconnection of theupper outer major chords 58, 59 to upper central major chord 57, and theconnection of auxiliary framing members to chords 58 and 59. Such a stepis depicted in FIG. 22 which shows upper minor chord framing members 61pinned between center chord node connectors 74 and laterally adjacentouter chord node connectors 75; in the interest of clarity ofillustration, frame elements located below the top of the frame are notshown in FIG. 22. Torsion braces 92 are disposed (one in each of the sixbays defined by members 57, 58, 59 and 61) diagonally between the chordmembers so that, on each side of center chord 57, the torsion bracesalternate in the ways which they are skewed relative to the length ofthe frame. As connected between major chords 57, 58 and 59, upper minorchords 61 can carry inverted U-clips 98 at selected locations alongtheir lengths for later connection to them of longitudinal mirrormounting tubes 99 (see FIGS. 23 and 24). Clips 98 function as risersfrom the flat upper surfaces of frame 50 to conform to the curvature ofthe focusing reflector which the frame supports in use. Also, squareextension tubes 100 (akin to frame outriggers) can be rigidly connectedbetween surfaces 87 of each of node connectors 75. Each tube 100 cancarry an inverted U-clip at its unsupported end. Thus, at eachtransverse station of frame 50 corresponding to the locations of upperminor chords 61, the frame can include six clips 98 as features whichfacilitate the connection of mirror 64 to the frame.

Attention is directed to node connector 74 on upper center major chord57 between plate 90 and the left end of the frame as depicted in FIGS.21, 22 and 23. In addition to major chord 57 which extends continuously(preferably) through that node connector, there are ten further framingmembers which have an end pinned to that node connector, namely, fourcentral struts 60 having end surfaces registered with node connectorsurfaces 81 and 82, two torsion braces 92 and one upper minor chord 61having end surfaces registered with connector surfaces 83, and twotorsion braces and one upper minor chord 61 having end surfacesregistered with connector surfaces 84. That plurality of framing memberconnections to that node connector illustrates one form of theversatility of node connectors according to this invention.

The presence of mirror support outriggers 100 in frame 50 illustratesanother form of the versatility of this invention's node connectors,namely, the ability of the node connectors to function as connectors forelements which are auxiliary to but not part of the relevant space frameas such.

FIGS. 23 and 24 show a plurality of mirror support tubes 99, disposed onparallel lines along the length of the frame, connected either directlyto frame 50 or to inverted U-clips 98 which are connected to the frame.The mirror support tubes 99 preferably are aluminum extrusions with across-sectional configuration which includes a rectangle or a squarewith upper and lower external flanges. The mirror support tubes conformto a curved line which is, in essence, the curvature of the reverse sideof concave mirror 64.

FIG. 23 is a top plan view of frame 50 with mirror support tubes mountedto it. FIG. 23 is a good illustration of the benefits of using extrudedor pultruded elements of constant cross-section and indefinite length assources for node connectors of specified cross-section but of differentlengths. For example, in FIG. 23 there are four node connectors 75carried on each of major chords 58 and 59; on each of those chords, thenode connectors are of three different lengths determined, principally,by the number of other framing members which are connected to them.

A torque arm 65 for mirror support frame 50 is shown in FIG. 25. Closelyadjacent to its upper end, a large aperture 102 is formed through theplate for cooperation with a frame drive shaft (not shown) which canpass through that aperture to a suitable mechanism for controllablyrotating the shaft. The plate provides a mechanism for connecting aframe 50 to such a drive shaft for movement of the frame with the shaft.Plate 65 also includes a smaller hole 103 through it below aperture 102,but near the upper end of the plate, for receipt of an end of frameupper central major chord 57. A cross piece 104 can be connected to thelower end of the plate and to define a pair of holes via which the platecan be bolted, e.g., to a coupling fitting 94 of frame 50.

As noted above, all framing members (major chords, minor chords, struts,torsion braces, and other components) and node connectors of frame 50preferably are made of the same type of aluminum. Thus, all of thoseframe components are affected equally by temperature changes. Also, allpinned connections in frame 50 preferably are defined by use of thezero-clearance shear pin technique described above. Precisionfabrication of the components of frame 50 for field assembly, includingcutting extrusions to desired lengths and the drilling (or other holeformation operations) of holes in those extrusion lengths at preciselocations can be facilitated by the use of precision jigs and fixturesand the use of appropriate shop practices. As a result, frame 50 can beconstructed to very small tolerances which produce a very rigid,comparatively lightweight, and temperature-insensitive support formirror 64 which manifests essentially no deflection as the frame isturned about its mounting axis and experiences changes in the waygravity acts on the frame.

Worked skilled in the art will appreciate that the cross-sectionalconfigurations of node connectors having chord-retaining tubularportions, such as portions 70 of node connectors 69, 74, and 75, can bevaried to define passages conforming to the cross-sectional shapes ofnon-round tubular members or of non-tubular members having standardshapes (e.g., channels) or custom shapes. Those workers also willappreciate that transverse chords, struts, and torsion braces can besquare or other even-sided polygons, ovals with flats, or rolled shapeshaving flat and parallel exterior surfaces.

The zero-clearance shear pins described above (see FIG. 11) can beinstalled, to make desired connections, either by driving them axiallyinto place through the relevant holes in node connectors and framingmembers, or by turning them into place. If the pertinent framing memberhas its pin receiving holes formed in relatively thick-walled portionsof the member, then the zero-clearance shear pin can be installed byaxially driving it, as by lightly hammering on the head of the pin; thepin shank preferably is lubricated before its installation is started.However, if the framing member is a thin walled tube, e.g., driving azero-clearance shear pin into place through those holes may producedimpling (or other undesired permanent distortion) of the framing memberin the vicinity of those holes. In that situation, the preferredprocedure for installing a lubricated zero-clearance shear pin in toturn it into position, as by use of a wrench engaged with a non-roundshear pin head, while applying axial force to the pin. In the lattersituation, the threadless shank of the shear pin “self-threads” its wayinto and through the framing member holes without causing dimpling orother distortion of the framing member in ways which can reduce theforce transmitting ability of the member as connected to its nodeconnector.

A space frame, once assembled, rarely has any of its connectionsdisassembled and removed. This invention affords the ability todisassemble and to reassemble a space frame having interconnectionsusing zero-clearance shear pins. An example of such a disassembablespace frame is scaffolding, and in such space frames (as well as others)the configuration of zero-clearance shear pin 110 shown in FIG. 26 canbe used to advantage. Pin 110 has a non-round head 111 at one end of anunthreaded round shank 112, so that the pin can be driven or turned toinstall it in or to remove it from a pinned connection. Rather thanbeing of constant diameter along its length (save for the presence of acircumferential clip retainer groove) as is pin 40 shown in FIG. 11, theshank 112 of pin 110 is of non-constant diameter. Shank 112 has arelatively short portion 113 of relatively large diameter adjacent toits head 111, and a relatively longer relatively small diameter portion114 along the balance of its length to a tapered distal end 115 of thepin. A circumferential clip retainer groove 116 is formed in shankposition 114 near the distal end of the shank. Preferably, theintersections of the groove walls with the shank's cylindrical surfaceare chamfered, as at 117, to make easier the insertion and removal ofpin 110 into and from thin-wall framing members. It will be apparentthat use of pin 110 requires that the pin receiving holes in the end ofa framing member be of different diameters, one having a diameter equalto the larger diameter of the pin and the other having a smallerdiameter equal to the smaller diameter of the pin. The differencebetween the larger and smaller diameter of pin shank 112 preferably isslight (e.g., on the order of 0.015 inch) so that the shear resistingcapacity of the pin is not meaningfully reduced in its smaller diameterportion, and so that the bearing area of the pin for a framing memberconnected by it is not meaningfully reduced. An advantage of pin 110 isthat its small diameter shank portion does not encounter a receivinghole of that diameter, in the course of being installed, until about thesame time as the large diameter portion of the shank encounters areceiving hole of that larger diameter. Installation of the pin to makea pinned connection is easier and faster. Also, in removing the pin froma zero-clearance pinned connection, both pin shank portions become freefrom their receiving holes at substantially the same time, making pinremoval easier and faster. A further benefit is the pin shank and thepin receiving holes in framing members are subjected to significantlyreduced episodes of wear of the pin and holes which can cause theireffective sizes to change as pinned connections are repeatedly made anddisassembled over time. Thus, the benefits of zero-clearance pinnedconnections can be achieved over longer times in scaffolding and otherspace frames which are subject to disassembly and reassembly.

Overall weight of a DLG-type space frame often is a significant designproblem, especially where the frame is to be subject in use tosignificant loads, static or dynamic. The use of thin wall framingmembers suggests itself as a solution to the weight problem. However,where framing members can be subject to meaningful axial loads andpinned connections are to establish framing member interconnections, theuse of thin wall framing members can be problematic and troublesome. Thereason is that thin wall tubular framing members, because of thethinness of their walls, afford only small areas of the membercross-sections for bearing against shear pins, and for transfer of axialloads in the framing member to a node connector via the shear pins.Those small bearing areas mean that axial forces in the framing memberare concentrated in those small areas as they transfer from the memberto the shear pin, and that stresses in the members are highest in thoseareas. Those stresses can reach sufficiently high levels that theframing member crumples, tears or otherwise very adversely deforms atits pin receiving holes, thereby enlarging the effective diameter ofthose holes. Enlargement of the diameter of a shear pin receiving holein a framing member of the space frame has the effect of changing theworking length of the member, and that means that the member no longercan carry or transmit the loads applied to it in the space frame. That,in turn, causes other framing members in the space frame to be subjectedto increased loads, which can cause their pin receiving holes to enlargeas those other framing members tear or crumple at those holes. Theresult can be a catastrophic failure of the space frame. FIGS. 27 and 28depict a solution to the problem of the use of thin wall tubes asframing members in reduced weight space frames.

FIG. 27 is a transverse cross-sectional elevation view of a non-round(oval) thin wall structural tube 120, preferably an extrusion. Over mostof its circumference, tube 120 has a relatively small wall thickness t₁.Tube 120 has orthogonally related (perpendicularly oriented) axes ofsymmetry X-X and Y-Y (or X and Y axes). The tube dimension along the Yaxis is less than its dimension along the X axis. The tubecross-sectional shape is arranged so that the tube has opposite walledflat exterior surface portions 121 which are centered on and extendacross the member's Y axis and are parallel to axis X, and in the widthof each of those surface portions 121 the wall thickness of the framingmembers is increased (preferably inwardly) to thickness t₂. That is, thespacing of the inner surface of the tube from its outer surfaceincreases from t₁ to t₂ across the width of each surface portion 121. Asa result, tube 120 has increased bearing areas against a shear pinpassing through pin receiving holes 122 formed through the tube inalignment with the Y axis. The increased bearing areas means that thetube can carry and transmit to the shear pin axial loads in the tube ofmagnitude greater than would cause a tube having uniform wall thicknesst₁ to crumple or tear at holes 122.

In tube 120, zones 121 of increased wall thickness extend along theentire length of the tube. It will be apparent that if the tube weredefined with uniform wall thickness around its circumference, thesection modulus of the tube (and its resistance to bending) about thetube's Y axis would be greater than the section modulus of the tube (andits resistance to bending) about the tube's X axis. It is also apparentthat, because the wall thickness of tube 120 is increased in theportions of the tube's circumference where the exterior surfaces of thetube are flat and parallel to the tube's X axis, tube 120 has a sectionmodulus about the X axis which is greater than the X axis sectionmodulus of a tube of the same exterior contour and dimension havinguniform wall thickness t₁ about its circumference, and so tube 120 ismore resistant to bending about the X axis than such comparable tube ofuniform wall thickness t₁. Thus, it will be apparent that by adjustmentof the widths of tube zones 121 and the difference between tube wallthickness t₁ and t₂, tube 120 can be defined to have a section modulusabout the X axis which is equal to the tube's section modulus about theY axis, so that the tube's structural performance abilities in bendingare essentially the same as those of a round tube having a diameterequal to the X axis dimension of tube 120 and having uniform wallthickness t₁. The thin wall tube 120 has enhanced ability to carry andtransmit axial loads (tension or compression) because of its increasedwall thickness at holes 122. Tube 120 also has enhanced columnproperties (notably resistance to buckling when subjected to compressiveloads) because of its enhanced section modulus about its X axis. Thesebenefits are obtained with minimal increase in the weight of the tubeover one of uniform wall thickness t₁ because the adjustments to wallthickness are made in small sections of the tube circumference wherethey are most effective. The presence of oppositely facing aligned, flatareas in the exterior of tube 120 adapts tube 120 to effective use innode connectors of this invention because those flat tube surfaces canregister closely with facing flat surfaces of a node connector where thetube can be pinned to the node connector. The ability to use thin walltubes, modified according to the principles illustrated in FIG. 27, in aspace frame having pinned connections means that the weights of framingmembers (major chords, minor chords, struts, torsion braces, and thelike) in such frames can be reduced without reducing the load carryingcapacity of the frame. Reductions in the weight of space framecomponents produce reductions in the costs of the frame components.

FIG. 28 is a transverse cross-section view of another non-round(rectangular) thin wall structural tube 125 which has its wall thicknessincreased to t₂ from t₁ in central zones 126 of its greater dimension(width along the tube's X axis, as compared to its height along the Yaxis.) The increased wall thickness preferably is manifested in theinner surfaces of tube 125. Shear pin receiving holes 127 are formedthrough the tube walls in its zones of increased wall thickness,preferably centered on the Y axis, adjacent each end of the tube so thatthe tube can be pinned to a node connector according to this inventionin a space frame of reduced weight. Tube 125, like tube 120, can be usedto define a major chord, a minor chord, a strut, or other component ofthe frame. Tube 125 can be defined to have equal section moduli aboutits X and Y axes, if desired, or unequal adjusted section moduli if thatshould be desired.

The node connectors 69, 74 and 75 shown in FIGS. 6, 8 and 10 havetubular base portions 70 defining passages 71 which fully encircle theround tubular chords with which they cooperate. While it is desirablethat the cross-sectional configuration of a node connector be such that,upon slidable insertion of a chord member into the connectors chordreceiving passage, the connector and the chord member cooperate so thatthe chord member is held in the connector with its axis substantiallyaligned with the passage axis, that objective can be attained by asuitably designed node connector having a passage which does not fullycircumferentially enclose the chord member. That is, the nodeconnector's chord receiving passage need not fully enclose the chordmember circumferentially in order that the node connector can receivethe chord member from moving sideways in the node connector. That aspectof this invention is illustrated in FIGS. 29, 30, and 31.

FIG. 29 is a transverse cross-section view of a node connector 130 whichcooperates with a tubular chord member 131 of non-round cross-section.Chord member 131 is predominantly round in cross-section but has alateral outward projection 132 which subtends about 90° of thecircumference of the otherwise round chord member. The projection iscomprised by a pair of short parallel outwardly extending flanges 133which connect to the opposite ends of a flat web or bridge 134. Thecross-section of the chord member is symmetrical about a plane throughthe axis (center of curvature) of the round portion of the chord tubeand perpendicular to the plane of the bridge at the mid-length of thebridge. The cross-sectional configuration of the preferably extrudednode connector 130 has a base portion of tubular nature defining apassage 135 which is sized and shaped so that, upon insertion of chordmember 131 endwise into the passage, the passage surfaces cooperateclosely with the outer surfaces of flanges 133 and the round majorportion of the chord adequately to hold the chord in the connector inthe desired way. Thus, the node connector has spaced parallel outwardlyextending ribs 136 which cooperate with the outer surfaces of projectionflanges 133, but between those ribs the passage has a lateral openingfrom it along its length to accommodate the chord member projection 132.The ends of ribs 136 lie in the plane of the top of projection 132 whenthe node connector and the chord member are engaged with each other.

The node connector 130 can be secured rigidly to chord member by passingshear pins through them adjacent to and parallel to the bottom of thechord member's bridge 133. Alternately, as shown in FIG. 29, theconnection of the node connector to the chord member can be made byengaging bolts 138 through holes in the node connector ribs into tappedholes in the chord member flanges 131.

Node connector 130 and chord member 131 can be components in the upperlayer of a classic flat DLG space frame of the kind shown in FIG. 1, asin an application of the space frame where the frame is to supportdecking or a roof arrangement. In that application, the chord member,due to its upward projection 132 along its length, has enhancedresistance to bending and so has properties akin to that of a beam. Foruse in such an application, outwardly extending elements (flanges) 77present along the length of the node connector can define pairs offacing spaced parallel flat surfaces 140, 141, 142 and 143 for receivingtransverse chords and struts of the frame. In each pair of surfaces, thefacing surfaces can be equidistant from opposite sides of a center planewhich includes the axis of passage 135. Surfaces 140 and 141 areparallel with respective ones of them coplanar; those surface pairs canreceive and have pinned to them the adjacent ends of two co-lineartransverse chords of the space frame. Surfaces 142 and 143 are angledout and down from each other; the elements defining those surface pairscan receive and have pinned between them ends of struts (two per surfacepair) which interconnect to four different nodes in the other (bottom)layer of the space frame.

FIG. 30 is a cross-section view of a node connector 139 which is avariant of node connector 130 and of a chord member 131. It was notedabove that node connector 130 has a plane of symmetry, namely a planevertically through the center of curvature of the round portion ofpassage 135 as node connector 130 is depicted in FIG. 29. The variationof node connector 139 upon node connector 130 is that both haveessentially the same cross-sectional configuration, but connector 139 isdefined by two identical parts 139A and 139B which are connectedtogether at the vertical plane of symmetry of connector 139. To enableparts 139A and 139B to be bolted together, as by bolts 140, each ofparts 139A and 139B has an exterior flange or rib 141, from which one ofelements 77 is carried, having a mating surface on the plane of symmetryof the assembled connector 139 and in which holes for bolts 140 areformed. Because parts 139A and 139B are identical in cross-section, theycan be made from a common extrusion. The two-part node connector 139,e.g., is advantageous if the total cross-sectional area and dimension ofthe overall connector is large; there is a limited number of largeextrusion presses in the world, and the two-part nature of connector 139means that extrusions for use in its construction can be made on smallerextrusion presses of which there are many.

FIG. 31 is a cross-section view of a node connector 145 and a tubularchord member 146 which cooperate with each other; connector 145 is amodest variant of connector 139, and chord member 146 is a modestvariant of chord member 131. The difference between the cross-sectionalconfigurations of chord members 131 and 146 is that chord member 146includes an external radial rib 148 along its length. The rib iscentered on the plane of symmetry of the chord member. The differencebetween identical parts 145A and 145B of connector 145 relative to theparts 139A and 149B of connector 139 is that the ribs 149 of parts 145Aand 145B are defined to mate with the opposite faces of chord member rib148 rather than with each other. Because of the presence of its externalrib 148, chord member 146 has enhanced beam properties over chord member131.

Comment was made above that a variant of node connector 130 (FIG. 29),in which the passage through the length is a round circumferentiallyclosed passage, can be used in the construction of a classic squareframe (see FIG. 1) in which the longitudinal major chords are round andother framing members can be square, oval with external flats, orotherwise consistent with the preceding descriptions. Such a variant ofnode connector 130 can be used to define the “free form” or laterallycurved DLG space frame 150 shown in FIGS. 32 (top plan view) and 33(side elevation view), simply by making the upper and lower transversechords 151 and 152 round and continuous through at least some of theframe nodes (splices may be needed) and by making the upper and lowerlongitudinal chord members 153 and 154 square and of lengthscorresponding to the distance along a longitudinal chord line betweenadjacent nodes. The existence of an ability to construct such alaterally curved DLG space frame is shown by FIG. 33, a side elevationof such a frame, in which struts lie in diagonal planes extending acrossthe width of the frame. The planes of the strut receiving surfaces 142and 143 of such a node connector so disposed in the frame would beparallel to transverse chord lines, all of which are straight anduniformly spaced from each other along the length of the frame. Struts155 connect between upper nodes 156 and lower nodes 157. Strutsconnected to a given node can have unequal lengths to accommodate thelateral displacements of adjacent transverse chord members needed toproduce the laterally curved plan shape of the frame shown in FIG. 32.

It is apparent, therefore, that a node connector according to thisinvention, in which the parallel surfaces between which struts anddiscontinuous chord members are connected are surfaces which areparallel to the length of the passages in which a continuous chordmember is received, is a node connector which can be used in a varietyof differently configured DLG space frames, including frames which haveuniform bay spacing longitudinally and transversely, space frames whichhave variable bay spacing longitudinally or transversely, and spaceframes in which longitudinal or transverse chord members are shiftedlaterally of each other as shown in FIG. 32.

Many benefits and advantages are afforded by this invention and itsaspects and features described above. The node connectors enable certainchords of a DLG space frame to extend continuously though them. The nodeconnectors can be used with space frame framing members of substantiallyany cross-sectional configuration desired; they are not limited to usewith members having round or rectangular cross-sections. Node connectorsand framing members can be extruded for low cost and dimensionalprecision. Node connectors and framing members can be made of materialshaving uniform metallurgical properties so that, among other benefits,space frames incorporating them are little affected dimensionally bytemperature changes. The node connectors enable framing members ofdiffering numbers, size and cross-sectional configuration to beeffectively interconnected at a given node in a space frame. The nodeconnectors can be defined to enable good, even ideal, positioning andalignment of framing members at a space frame node so that there areminimal or no eccentricities of framing member axes relative to eachother at a node. The node connectors enable convenient use of variablebay spacing in a space frame, enabling the overall frame to efficientlycarry design loads. The node connectors can be defined to provideinterconnections between framing members in a diverse range of positionsand numbers, thus enabling the use of DLG design and constructionprinciples in more complex structures including non-static (movable)structures for electro-magnetic radiation focusing applications such asmovable mirror or reflector support armatures in solar power generationfacilities and in radio and optical telescopes. Use-specific elementscan be accommodated in space frames, such as mountings for solarreflectors, torque members, and other supports and accessories.

The zero-clearance shear pin connection aspects of this invention enableprecision connections in space frames to be easily and inexpensivelymade, while also enabling other frame components to correctly performassigned load carrying functions. Such connections can be disassembledand reassembled plural times while retaining desired levels of precisionand tightness. The shear pins can be driven or turned into and out ofinstalled positions in other members. Also, as explained with referencesto FIGS. 27 and 28, aspects of this invention enable minimum weightframing members to have enhanced axial load transmitting capabilities inpinned connections. The invention also enables a tubular structuralelement which is asymmetrical in X and Y directions to have equal (orother desired tailored) section moduli about those axes, therebyenabling weight saving thin wall tubes to be used to increased advantagein space frames.

The foregoing descriptions of depicted and other aspects of thisinvention are to be read as illustrative explanations to persons havingskill in the relevant arts and technologies, not as an exhaustivecatalog of all structural and procedural forms in which the inventioncan be embodied or used to advantage. Variations of the describedstructures and procedures can be used without departing from the fairscope of the invention.

1. In a pinned connection of an end of a framing member in a doublelayer grid-type of space frame at a node of the frame via a nodeconnector having elements which define a pair of spaced parallelsubstantially flat opposing surfaces, the framing member end beingdisposed between the opposing element surfaces of the node connector andhaving substantially flat substantially parallel opposite exteriorsurfaces, a shear pin receiving passage through the framing member endalong a line substantially normal to the framing member parallelexterior surfaces, a pair of holes through the node connector elementsaligned on a line substantially normal to the pair of opposing surface,and a shear pin insertable through the holes and the passage uponsuitable placement of the framing member end between the opposingelement surface, the improvement in which the shear pin is defined tohave substantially an interference fit within the holes and the passageupon insertion of the pin into the holes and the passage.
 2. Apparatusaccording to claim 1 in which the shear pin has a head structure at oneend thereof at an end of a round pin shank, the shank having a largerdiameter portion adjacent the head and a smaller diameter portion at andadjacent to the other end of the shank, and the holes in the nodeconnector elements have different diameters corresponding to the largerand smaller diameters of the pin shank.
 3. Apparatus according to claim2 in which the framing member is tubular in nature and the passagethrough its end is defined by a pair of holes which have differentdiameters corresponding to the larger and smaller diameters of the pinshank.
 4. Apparatus according to claim 1 in which the pin diameter ineach framing member hole is oversize relative to the pin diameterrequired to resist shearing of the pin under design axial loads in theframing member applied to the pin.
 5. Apparatus according to claim 2 inwhich the head of the pin is configured for cooperation with a tool bywhich torque can be applied.
 6. Apparatus according to claim 1 in whichthe pin is devoid of threads.
 7. Apparatus according to claim 1 in whichthe framing member is tubular and is of increased wall thickness alongits length at opposing locations on the members, the passage beingdefined as aligned holes through the locations of increased wallthickness of the framing member.